Flight simulation and testing of the FanWing experimental aircraft

Abstract

Purpose

This paper aims to create an accurate computer‐based flight simulation of the FanWing experimental aircraft. The model would then be used to record and document the aircraft's performance and handling qualities.

Design/methodology/approach

The project consisted of three phases. The first was to simplify and convert existing aerodynamic data into a form that was compatible with the simulation software. The second phase involved the development of the model, and the third, flight testing.

Findings

The aircraft performance and handling qualities of the aircraft were recorded in all flight phases.

Research limitations/implications

The FanWing's aerodynamics are unusual and software limitations prevented its characteristics from being implemented directly. This meant that certain flight tests could not be carried out accurately.

Practical implications

The model will likely be used as a preliminary training tool for the FanWing's first pilots. It is also a useful publicity tool for the aircraft, and provides an insight into how this unusual aircraft flies, from a pilot's perspective.

Originality/value

Prior to this research, only aerodynamic data had documented the aircraft's performance. The simulation model allowed for conventional flight data to be recorded, and compared with similar aircraft.

Citation

Ahad, O. and Graham, J.M.R. (2007), "Flight simulation and testing of the FanWing experimental aircraft", Aircraft Engineering and Aerospace Technology, Vol. 79 No. 2, pp. 131-136. https://doi.org/10.1108/00022660710732671